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    Characteristics of Partial Length Circular Pin Fins As Heat Transfer Augmentors for Airfoil Internal Cooling Passages

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 559
    Author:
    S. C. Arora
    ,
    W. Abdel-Messeh
    DOI: 10.1115/1.2927694
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Pin fins are commonly used as heat transfer augmentors for internal cooling of turbine airfoils. These pins may extend from one wall to the other or may be segmented to meet specific requirements of removing the airfoil’s varying heat load. Three configurations of the partial pins were tested in a channel with aspect ratio 25:1 and the results are compared with those for the full pins. The array average heat transfer rate decreases linearly with increasing gap and is bounded by the value for full pins at one end and that for the smooth channel at the other. However, the local distribution of the Nusselt number and the average for each of the two walls depends on the configuration of the partial pins. The friction factor was lower for partial pins than for the full pins and also decreased with increasing gap. For the configuration with all partial pins on one wall, the friction factor was found to be the lowest, with no change in the corresponding heat transfer rate from a wall with pins.
    keyword(s): Heat transfer , Cooling , Fins , Airfoils , Pins (Engineering) , Friction , Channels (Hydraulic engineering) , Stress , Heat AND Turbines ,
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      Characteristics of Partial Length Circular Pin Fins As Heat Transfer Augmentors for Airfoil Internal Cooling Passages

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107748
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    • Journal of Turbomachinery

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    contributor authorS. C. Arora
    contributor authorW. Abdel-Messeh
    date accessioned2017-05-08T23:34:07Z
    date available2017-05-08T23:34:07Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#559_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107748
    description abstractPin fins are commonly used as heat transfer augmentors for internal cooling of turbine airfoils. These pins may extend from one wall to the other or may be segmented to meet specific requirements of removing the airfoil’s varying heat load. Three configurations of the partial pins were tested in a channel with aspect ratio 25:1 and the results are compared with those for the full pins. The array average heat transfer rate decreases linearly with increasing gap and is bounded by the value for full pins at one end and that for the smooth channel at the other. However, the local distribution of the Nusselt number and the average for each of the two walls depends on the configuration of the partial pins. The friction factor was lower for partial pins than for the full pins and also decreased with increasing gap. For the configuration with all partial pins on one wall, the friction factor was found to be the lowest, with no change in the corresponding heat transfer rate from a wall with pins.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCharacteristics of Partial Length Circular Pin Fins As Heat Transfer Augmentors for Airfoil Internal Cooling Passages
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927694
    journal fristpage559
    journal lastpage565
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsCooling
    keywordsFins
    keywordsAirfoils
    keywordsPins (Engineering)
    keywordsFriction
    keywordsChannels (Hydraulic engineering)
    keywordsStress
    keywordsHeat AND Turbines
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
    contenttypeFulltext
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